发明名称 Fan blade for a gas turbine engine
摘要 An injection-moulded thermoplastic mini-platform ( 42 ) is adhesively bonded, in use, to the aerofoil surfaces of a fan blade ( 312 ) in a gas turbine engine. The mini-platform ( 42 ) is divided into a number of leaves ( 46 ), to increase its flexibility, and ribs ( 48 ) beneath the leaves ( 46 ) provide additional stiffness in the radial direction. In the event that a fan blade is released in operation, the mini-platform ( 42 ) is designed to detach from the blade ( 312 ) and/or to break apart, so that damage to other components of the engine is minimised.
申请公布号 US2008159866(A1) 申请公布日期 2008.07.03
申请号 US20070819094 申请日期 2007.06.25
申请人 ROLLS-ROYCE PLC 发明人 EVANS DALE E.
分类号 F01D5/12 主分类号 F01D5/12
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